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Space Access Systems Design: Synthes...
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Rana, Loveneesh.
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Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems./
作者:
Rana, Loveneesh.
出版者:
Ann Arbor : ProQuest Dissertations & Theses, : 2017,
面頁冊數:
240 p.
附註:
Source: Dissertation Abstracts International, Volume: 79-09(E), Section: B.
Contained By:
Dissertation Abstracts International79-09B(E).
標題:
Aerospace engineering. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10833442
ISBN:
9780355912395
Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
Rana, Loveneesh.
Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
- Ann Arbor : ProQuest Dissertations & Theses, 2017 - 240 p.
Source: Dissertation Abstracts International, Volume: 79-09(E), Section: B.
Thesis (Ph.D.)--The University of Texas at Arlington, 2017.
This item is not available from ProQuest Dissertations & Theses.
The early Conceptual Design (CD) of a Space Access System (SAS) is the most abstract, innovative, and technologically challenging phase throughout the entire aerospace product development life-cycle. While it is the most important life-cycle phase which influences around 80 percent of the overall life-cycle-cost, it is also the least understood design phase. The history of space access vehicle design provides numerous examples of projects that failed due to lack of a proper technology-hardware-mission assessment in the CD phase. The present dissertation addresses this crucial phase and develops a prototype best practice solution process to advance the current state of the art of the CD oriented vehicle design synthesis systems. The solution is a generic process that can be applied to all categories of the SAS. The Vertical-Takeoff Horizontal-Landing type SAS is selected as the demonstration case-study for the solution process. The research provides a proof of concept for how the proposed prototype solution process expands the scope and application of current applications of the CD assessment vertically across the SAS system`s hierarchy and horizontally across the life-cycle phases of the SAS.
ISBN: 9780355912395Subjects--Topical Terms:
1002622
Aerospace engineering.
Space Access Systems Design: Synthesis Methodology Development for Conceptual Design of Future Space Access Systems.
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The early Conceptual Design (CD) of a Space Access System (SAS) is the most abstract, innovative, and technologically challenging phase throughout the entire aerospace product development life-cycle. While it is the most important life-cycle phase which influences around 80 percent of the overall life-cycle-cost, it is also the least understood design phase. The history of space access vehicle design provides numerous examples of projects that failed due to lack of a proper technology-hardware-mission assessment in the CD phase. The present dissertation addresses this crucial phase and develops a prototype best practice solution process to advance the current state of the art of the CD oriented vehicle design synthesis systems. The solution is a generic process that can be applied to all categories of the SAS. The Vertical-Takeoff Horizontal-Landing type SAS is selected as the demonstration case-study for the solution process. The research provides a proof of concept for how the proposed prototype solution process expands the scope and application of current applications of the CD assessment vertically across the SAS system`s hierarchy and horizontally across the life-cycle phases of the SAS.
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